US9753053B2 - Wind velocity sensor for a vehicle - Google Patents

Wind velocity sensor for a vehicle Download PDF

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Publication number
US9753053B2
US9753053B2 US14/718,617 US201514718617A US9753053B2 US 9753053 B2 US9753053 B2 US 9753053B2 US 201514718617 A US201514718617 A US 201514718617A US 9753053 B2 US9753053 B2 US 9753053B2
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Prior art keywords
guard member
platform
sensor according
ultrasonic sensors
wind
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US14/718,617
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US20160341757A1 (en
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Christopher M. Masucci
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Deere and Co
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Deere and Co
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Priority to US14/718,617 priority Critical patent/US9753053B2/en
Priority to AU2016264113A priority patent/AU2016264113B2/en
Priority to EP16797181.1A priority patent/EP3298356B1/en
Priority to PCT/US2016/032971 priority patent/WO2016187245A1/en
Priority to ES16797181T priority patent/ES2786556T3/es
Priority to BR112017018475-3A priority patent/BR112017018475B1/pt
Publication of US20160341757A1 publication Critical patent/US20160341757A1/en
Publication of US9753053B2 publication Critical patent/US9753053B2/en
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    • GPHYSICS
    • G01MEASURING; TESTING
    • G01PMEASURING LINEAR OR ANGULAR SPEED, ACCELERATION, DECELERATION, OR SHOCK; INDICATING PRESENCE, ABSENCE, OR DIRECTION, OF MOVEMENT
    • G01P5/00Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft
    • G01P5/24Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring the direct influence of the streaming fluid on the properties of a detecting acoustical wave
    • G01P5/245Measuring speed of fluids, e.g. of air stream; Measuring speed of bodies relative to fluids, e.g. of ship, of aircraft by measuring the direct influence of the streaming fluid on the properties of a detecting acoustical wave by measuring transit time of acoustical waves

Definitions

  • This disclosure relates to a wind velocity sensor for a vehicle.
  • Prior art wind velocity sensors can be mounted on vehicles to estimate wind velocity.
  • certain prior art wind sensors exhibit significant measuring error when an off-road vehicle moves in a work area or field.
  • a wind velocity sensor comprises a lower platform and an upper platform. Pillars are positioned or connected between the upper platform and the lower platform. Ultrasonic sensors are secured to corresponding ones of the pillars. A lower guard member extends outwardly from a reference ultrasonic sensor by a radial distance greater than a radial separation between any pair of the ultrasonic sensors.
  • FIG. 1 is a perspective view of a first embodiment of the wind velocity sensor.
  • FIG. 2 is a perspective view of a second embodiment of the wind velocity sensor.
  • FIG. 3 is a block diagram of a the electronic assembly of the wind velocity sensor of FIG. 1 or FIG. 2 .
  • a wind velocity sensor 11 comprises a lower platform 32 and an upper platform 34 . Pillars 40 are positioned or connected between the upper platform 34 and the lower platform 32 . Ultrasonic sensors ( 10 , 12 ) are secured to corresponding ones of the pillars 40 . A lower guard member 38 extends outwardly from a reference ultrasonic sensor 10 by a radial distance 103 greater than a radial separation 101 between any pair of the ultrasonic sensors ( 10 , 12 ).
  • turbulence created by the vehicle's irregular shape can distort or change the airflow detected by one or more ultrasonic sensors ( 10 , 12 ), which can cause it or them to read inaccurate wind velocity, including the wind direction, the magnitude of the wind speed, or both.
  • the lower guard member 38 is positioned below the ultrasonic sensors ( 10 , 12 ) and the upper guard member 36 is positioned above the ultrasonic sensor to straighten and guide the airflow detected by one or more sensors ( 10 , 12 ), while deflecting turbulence from above or below the guard members ( 36 , 38 ).
  • a lower platform 32 comprises a substantially cylindrical structure, a substantially polygonal structure, or substantially rectangular structure.
  • the upper platform 34 comprises a substantially cylindrical structure, a substantially polygonal structure, or substantially rectangular structure.
  • Either the lower platform 32 or the upper platform 34 may be formed by joining a first housing member and a second housing member to house an electronics assembly 112 , save the ultrasonic sensors ( 10 , 12 ).
  • electronics assembly 112 is illustrated in dashed or phantom lines in FIG. 1 within the lower platform 32 , although other embodiments can fall within the scope of the appended claims. The electronics assembly 112 is described in more detail in conjunction with FIG. 3 .
  • a set pillars 40 are positioned between or connected to the upper platform 34 and the lower platform 32 .
  • each pillar may have any cross-sectional shape such as substantially elliptical, rectangular, triangular, or otherwise.
  • each pillar 40 has a notch or recess (e.g., semi-cylindrical notch) for receiving or mounting a corresponding ultrasonic sensor within the notch or recess.
  • the ultrasonic sensors ( 10 , 12 ) are secured to corresponding ones of the pillars 40 by fasteners, a snap-fit connection, or adhesive bonding, for example. At least two ultrasonic sensors 10 are required to provide an estimate wind velocity, although three or more ultrasonic sensors ( 10 , 12 ) can provide more accurate estimates. Ultrasonic sensors 12 are shown as dashed lines in FIG. 1 , FIG. 2 and FIG. 3 because the ultrasonic sensors are optional.
  • a lower guard member 38 extends outwardly by a radial distance 103 that is substantially equal to the radial distance 103 of the upper guard member 36 .
  • the lower guard member 38 extends outwardly from a reference ultrasonic sensor 10 (or any arbitrary ultrasonic sensor) by greater radial distance 103 than a radial separation 101 between any pair of the ultrasonic sensors ( 10 , 12 ).
  • the upper guard member 36 extends outwardly from an ultrasonic sensor ( 10 , 12 ) by a radial distance 103 greater than a radial separation 101 between any pair of the ultrasonic sensors ( 10 , 12 ). If the ultrasonic sensor is co-located with a pillar 40 , the radial distance 103 and the radial separation 101 may be measured from a central vertical axis 55 of each pillar 40 , for example.
  • the upper guard member 36 and the lower guard member 38 may have virtually any perimeter shape (e.g., curved, circular, elliptical, ring-shaped, scalloped, or polygonal) so long as the upper guard member 36 and the lower guard member 38 are substantially planar or generally flat. As illustrated, in FIG. 1 , the upper guard member 36 is substantially annular and substantially planar. Similarly, the lower guard member 38 is substantially annular and substantially planar. In certain embodiments, the upper guard member 36 may be referred to as a disc or disc-shaped member; the lower guard member 38 may be referred to as a disc or disc-shaped member.
  • the upper guard member 36 is secured to at least a portion of a lower surface 38 of the upper platform 34 .
  • the upper guard member 36 is adhesively bonded to at least a portion (e.g., an outer ring surface) of the lower surface 38 of the upper platform 34 .
  • the lower guard member 38 is secured to at least a portion of an upper surface 35 (e.g., an outer ring surface) of the lower platform 32 .
  • the lower guard member 38 is adhesively bonded to at least a portion of the lower surface 35 of the upper platform 34 .
  • the wind velocity sensor 11 is capable of mounting on a vehicle or implement, or a stationary structure.
  • the wind velocity sensor 11 is well suited for mounting on agricultural, construction, forestry and other off-road work vehicles, or its or their associated implements.
  • One end of a support shaft 44 is connected to the lower platform 32 and an opposite end of the support shaft has a flange 46 for connection to the vehicle, implement, or other structure 48 via one or more fasteners 50 .
  • the wind velocity sensor 111 of FIG. 2 is similar to the wind velocity sensor 11 of FIG. 1 , except in FIG. 2 each of the upper guard member 136 and the lower guard member 138 has a shoulder, collar or hub. Like elements in FIG. 1 and FIG. 2 are indicated by like reference numbers.
  • the upper guard member 136 has a shoulder, collar or hub 52 for mating with an outer perimeter of the upper platform 34 and the lower guard member 138 has a shoulder, collar or hub 52 for mating with an outer perimeter of the lower platform 32 .
  • the shoulder, collar or hub 52 is press-fitted onto the outer perimeter of the upper platform 34 to secure the upper guard member 136 to the upper platform 34 .
  • the shoulder, collar or hub 52 is press-fitted onto the outer perimeter of the lower platform 32 to secure the upper guard member 136 to the lower platform 32 .
  • the shoulder, collar or hub 52 of the lower guard member 138 or the upper guard member 136 may be adhesively bonded, welded, or fastened (with fasteners) to the lower guard platform or the upper guard platform, respectively.
  • the lower platform 32 , the upper platform 34 , or both may comprise an electronics enclosure with a first enclosure portion and a mating second enclosure portion that encloses the electronic assembly 112 illustrated in the block diagram.
  • the first enclosure may nest with the second enclosure portion, or the first enclosure portion may comprise a lid for mounting on a container that embodies the second enclosure portion.
  • the electronics assembly 112 has one or more ultrasonic sensors ( 10 , 12 ) that are arranged to sense or detect wind velocity.
  • the ultrasonic sensors ( 10 , 12 ) are positioned in association with corresponding pillars 40 as illustrated in FIG. 1 or FIG. 2 , for example.
  • Each ultrasonic sensor ( 10 , 12 ) comprises an ultrasonic transducer that has sensor terminals.
  • a driver 16 is coupled to the sensor terminals to drive the ultrasonic sensor ( 10 , 12 ) to produce or transmit a sound pulse or noise pulse at the transmission time.
  • Each ultrasonic sensor ( 10 , 12 ) can generate or transmit a sound pulse or noise pulse within a measurement frequency band (e.g., approximately 150 Hz to approximately 450 kHz).
  • Each ultrasonic sensor ( 10 , 12 ) can receive, detect or sense a sound pulse or noise pulse within a measurement frequency band (e.g., approximately 150 Hz to approximately 450 kHz).
  • Input terminals of the multiplexer 14 are coupled to the sensor terminals of one or more ultrasonic sensors ( 10 , 12 ).
  • the multiplexer 14 receives received signals that contain reception time measurements and other signal parameters (e.g., magnitude and frequency shift) of sound pulses from one or more ultrasonic sensors ( 10 , 12 ).
  • the multiplexer 14 output is fed to an analog-to-digital converter 18 that receives signals from one or more of the ultrasonic sensors ( 10 , 12 ) via the multiplexer 14 .
  • An electronic data processor 26 comprises a microcontroller, a microprocessor, a programmable gate array, an application specific integrated circuit, a digital signal processor, or another data processor for storing, retrieving, manipulating or processing data.
  • the data processor 26 is coupled to a data bus 24 .
  • the data bus 24 is connected to one or more data ports 22 and a data storage device 30 .
  • the data storage device 30 comprises an electronic memory, nonvolatile random access memory, a magnetic storage device, an optical storage device, a hard disc drive, or the like.
  • the data storage device 30 may store software or instructions that can be executed by the data processor 26 .
  • the data storage device 30 may storage a wind velocity estimator 28 .
  • the data processor 26 or wind velocity estimator 28 reads reception time measurements and other signal parameters (e.g., magnitude or frequency shift) of sound pulses from one or more ultrasonic sensors ( 10 , 12 ) on a time-slot multiplexed basis.
  • the data processor 26 or wind velocity estimator 28 determines a time difference between a transmission time of the sound pulse from one ultrasonic sensor ( 10 , 12 ) and reception time of the transmitted noise pulse at the other ultrasonic sensors ( 10 , 12 ) provides an indication of wind velocity, including wind direction and wind speed.
  • the wind direction requires the wind sensor ( 11 , 111 ) to be oriented with a known direction to North heading or that the vehicle heading is known for a vehicle-mounted wind velocity sensor ( 11 or 111 ).
  • a location-determining receiver 20 may provide location data 17 , heading data 19 , or both to the data processor 26 such that the data processor 26 can compensate for a vehicle movement vector.
  • the data processor 26 can subtract the vehicle movement vector from an estimated wind velocity vector, to negate the effect of the vehicle heading on the orientation to North of the wind velocity sensor ( 11 or 111 ).
  • the data processor 26 or wind velocity estimator 28 is programmed or arranged to process the received signals to provide an estimate of the wind velocity vector based on the measurements from the ultrasonic sensors ( 10 , 12 ) and the location data 17 and heading data 19 from the location-determining receiver 20 .
  • the data processor 26 can measure the transmission time of sound pulses, the corresponding reception time of the transmitted sound pulses at one or more ultrasonic sensors ( 10 , 12 ), and the magnitude or other signal parameters.

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  • Physics & Mathematics (AREA)
  • Engineering & Computer Science (AREA)
  • Acoustics & Sound (AREA)
  • Multimedia (AREA)
  • Aviation & Aerospace Engineering (AREA)
  • General Physics & Mathematics (AREA)
  • Indicating Or Recording The Presence, Absence, Or Direction Of Movement (AREA)
US14/718,617 2015-05-21 2015-05-21 Wind velocity sensor for a vehicle Active 2035-08-17 US9753053B2 (en)

Priority Applications (6)

Application Number Priority Date Filing Date Title
US14/718,617 US9753053B2 (en) 2015-05-21 2015-05-21 Wind velocity sensor for a vehicle
ES16797181T ES2786556T3 (es) 2015-05-21 2016-05-18 Sensor de velocidad del viento para un vehículo
EP16797181.1A EP3298356B1 (en) 2015-05-21 2016-05-18 Wind velocity sensor for a vehicle
PCT/US2016/032971 WO2016187245A1 (en) 2015-05-21 2016-05-18 Wind velocity sensor for a vehicle
AU2016264113A AU2016264113B2 (en) 2015-05-21 2016-05-18 Wind velocity sensor for a vehicle
BR112017018475-3A BR112017018475B1 (pt) 2015-05-21 2016-05-18 Sensor de velocidade de vento

Applications Claiming Priority (1)

Application Number Priority Date Filing Date Title
US14/718,617 US9753053B2 (en) 2015-05-21 2015-05-21 Wind velocity sensor for a vehicle

Publications (2)

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US20160341757A1 US20160341757A1 (en) 2016-11-24
US9753053B2 true US9753053B2 (en) 2017-09-05

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US14/718,617 Active 2035-08-17 US9753053B2 (en) 2015-05-21 2015-05-21 Wind velocity sensor for a vehicle

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US (1) US9753053B2 (pt)
EP (1) EP3298356B1 (pt)
AU (1) AU2016264113B2 (pt)
BR (1) BR112017018475B1 (pt)
ES (1) ES2786556T3 (pt)
WO (1) WO2016187245A1 (pt)

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Publication number Priority date Publication date Assignee Title
CN110018327A (zh) * 2019-04-11 2019-07-16 易泽雄 一种超声波测风仪及测风速方法
CN110988392B (zh) * 2019-11-11 2021-12-14 安徽理工大学 一种煤矿井下使用的超声波风速传感器
CN112649897B (zh) * 2020-10-10 2023-04-14 中国人民解放军空军研究院战场环境研究所 一种手持气象仪及风速和风力的测定方法

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US4890488A (en) 1988-03-03 1990-01-02 Simecsol Ultrasonic anemometer
US5343744A (en) 1992-03-06 1994-09-06 Tsi Incorporated Ultrasonic anemometer
US5877416A (en) 1996-04-13 1999-03-02 Ft Technologies Limited Anemometer employing standing wave normal to fluid flow and travelling wave normal to standing wave
US6370949B1 (en) 1999-09-14 2002-04-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Extreme wind velocity measurement system
JP2005249565A (ja) 2004-03-04 2005-09-15 Kanagawa Prefecture 風速計
US7269537B1 (en) 2005-02-26 2007-09-11 Duane Loren Mattern Infrasound sensor with disturbance filtering
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EP2600159A4 (en) 2010-07-30 2014-02-19 Pioneer Corp WIND DETECTION DEVICE
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US4890488A (en) 1988-03-03 1990-01-02 Simecsol Ultrasonic anemometer
US5343744A (en) 1992-03-06 1994-09-06 Tsi Incorporated Ultrasonic anemometer
US5877416A (en) 1996-04-13 1999-03-02 Ft Technologies Limited Anemometer employing standing wave normal to fluid flow and travelling wave normal to standing wave
US6370949B1 (en) 1999-09-14 2002-04-16 The United States Of America As Represented By The Administrator Of The National Aeronautics And Space Administration Extreme wind velocity measurement system
JP2005249565A (ja) 2004-03-04 2005-09-15 Kanagawa Prefecture 風速計
US7269537B1 (en) 2005-02-26 2007-09-11 Duane Loren Mattern Infrasound sensor with disturbance filtering
JP2014224719A (ja) * 2013-05-15 2014-12-04 本田技研工業株式会社 車両用風向き風速検出装置
US20150016223A1 (en) * 2013-07-15 2015-01-15 Qualcomm Incorporated Sensor array with receiver bias electrode

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Also Published As

Publication number Publication date
EP3298356A1 (en) 2018-03-28
BR112017018475A2 (pt) 2019-11-12
BR112017018475B1 (pt) 2021-04-06
WO2016187245A1 (en) 2016-11-24
ES2786556T3 (es) 2020-10-13
EP3298356A4 (en) 2019-01-02
AU2016264113B2 (en) 2021-04-22
US20160341757A1 (en) 2016-11-24
EP3298356B1 (en) 2020-02-05
AU2016264113A1 (en) 2017-12-07

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